TITLE input4_1.asc: UAV Uncontrolled flight
// Input for Lab4, HandsOn4_1
// Free flight (alpha=0, phivmx=0) with constant thrust
OPTIONS y_scrn n_comscrn n_events n_tabout y_plot y_traj n_merge y_doc 
MODULES
	environment		def,init,exec
	aerodynamics	def,exec	
	propulsion		def,init,exec	
	forces			def,exec	
	newton			def,init,exec	
END
TIMING
	scrn_step 2
	plot_step 0.1
	traj_step 0.5
	int_step 0.05
END
VEHICLES 1
	CRUISE3 UAV
		//Initial conditions
			lonx  14.7    //Vehicle longitude - deg  module newton
			latx  35.4    //Vehicle latitude - deg  module newton
			alt  7000    //Vehicle altitude - m  module newton
			psivgx  90    //Vehicle heading angle - deg  module newton
			thtvgx  0    //Vehicle flight path angle - deg  module newton
			dvbe  200    //Vehicle speed - m/s  module newton
		//Aerodynamics
			AERO_DECK cruise3_aero_deck.asc
		//Mass properties and propulsion
			mprop  1    //'int' Mode switch - ND  module propulsion
			mass_init  1000    //Initial vehicle mass - kg  module propulsion
			fuel_init  150    //Initial fuel - kg  module propulsion
			PROP_DECK cruise3_prop_deck.asc
			thrust_com  445    //Commanded thrust - N  module propulsion
	END
END
ENDTIME 20
STOP
